A method for the design of attitude control systems for flexible spacecraft is presented. The design procedure employs input-output linearization and stabilization techniques; computation of the sampled-data control laws, and compensation techniques are applied to reduce the influence of the flexible part on the control system design. An idealized test vehicle subject to a variety of control laws was simulated. The improvements obtained by using a sampled-data scheme with an extended control are evident from the results of the simulations.


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    Titel :

    Sampled Nonlinear Control for Large Angle Maneuvers of Flexible Spacecraft


    Beteiligte:
    S. Monaco (Autor:in) / D. N. Cyrot (Autor:in) / S. Stornelli (Autor:in)

    Erscheinungsdatum :

    1986


    Format / Umfang :

    8 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch






    Modeling and Control of a Flexible Spacecraft for Large-Angle Rapid Maneuvers

    Li, Y. / International Federation of Automatic Control | British Library Conference Proceedings | 1999